View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 64561U 26145.26748044 +.00000000 +00000-0 +48388-3 0 00002
2 64561 97.7713 260.3105 0001748 105.6560 254.4854 14.95955050 03
| Epoch (UTC): | 25 May 2026 06:25:10 |
| Eccentricity: | 0.0001748 |
| inclination: | 97.7713° |
| perigee height: | 578 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 260.3105° |
| argument of perigee: | 105.6560° |
| revolutions per day: | 14.95955050 |
| mean anomaly at epoch: | 254.4854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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